Solar panel

ABSTRACT

A high efficiency configuration for a solar cell module comprises solar cells arranged in an overlapping shingled manner and conductively bonded to each other in their overlapping regions to form super cells, which may be arranged to efficiently use the area of the solar module. Rear surface electrical connections between solar cells in electrically parallel super cells provide alternative current paths (i.e., detours) through the solar module around damaged, shaded, or otherwise underperforming solar cells.

CROSS REFERENCE TO RELATED APPLICATIONS

This application is a continuation of U.S. patent application Ser. No.16/111,578 filed Aug. 24, 2018, which is a continuation of U.S. patentapplication Ser. No. 15/210,516 titled “Solar Panel” and filed Jul. 14,2016, which claims benefit of priority to U.S. Provisional ApplicationNo. 62/206,667 titled “Solar Panel” filed Aug. 18, 2015. Each of theforegoing applications is incorporated herein by reference in itsentirety.

FIELD OF THE INVENTION

The invention relates generally to solar cell modules in which the solarcells are arranged in a shingled manner, and more particularly to suchsolar modules in which rear surface electrical connections between solarcells in electrically parallel rows of solar cells provide detourcurrent paths through the solar module around any underperforming solarcells.

BACKGROUND

Alternate sources of energy are needed to satisfy ever increasingworld-wide energy demands. Solar energy resources are sufficient in manygeographical regions to satisfy such demands, in part, by provision ofelectric power generated with solar (e.g., photovoltaic) cells.

SUMMARY

In one aspect, a solar module comprises a plurality of super cellsarranged in two or more physically parallel rows with the rowselectrically connected to each other in parallel. Each super cellcomprises a plurality of rectangular silicon solar cells arranged inline with long sides of adjacent silicon solar cells overlapping andconductively bonded directly to each other to electrically connect thesilicon solar cells in series. The solar module also comprises aplurality of detour electrical interconnects each of which is arrangedto extend perpendicularly to the rows of super cells to electricallyconnect rear surfaces of at least one pair of solar cells locatedside-by-side in adjacent rows to provide detour current paths throughthe module around one or more other solar cells in the event that theone or more other solar cells provide insufficient current for normaloperation of the module. These detour current paths do not pass throughbypass diodes.

These and other embodiments, features and advantages of the presentinvention will become more apparent to those skilled in the art whentaken with reference to the following more detailed description of theinvention in conjunction with the accompanying drawings that are firstbriefly described.

BRIEF DESCRIPTION OF THE DRAWINGS

FIG. 1 shows a cross-sectional diagram of a string of series-connectedsolar cells arranged in a shingled manner with the ends of adjacentsolar cells overlapping to form a shingled super cell.

FIG. 2 shows a diagram of the front surface of an example rectangularsolar module comprising a plurality of rectangular shingled super cells,with the long side of each super cell having a length of approximatelythe full length of the long side of the module. The super cells arearranged with their long sides parallel to the long sides of the module.

FIGS. 3-11 show diagrams of the rear surfaces of example solar modulesin which electrical interconnections between rear surfaces of solarcells in adjacent rows of super cells provide alternative current paths(i.e., detours) through the solar module around damaged, shaded, orotherwise underperforming solar cells.

FIGS. 12A-12B show rear surface metallization of individual solar cellsand detour electrical connections between super cells allowing currentto flow around a horizontal crack in a solar cell.

FIG. 13 shows a typical crack pattern in a conventional solar moduleafter uniform mechanical loading.

FIG. 14A shows an example patterned metallized back sheet that provideselectrical connections corresponding to those provided by the electricalinterconnects and return wires shown in FIG. 10 . FIG. 14B shows aclose-up view of electrical interconnections to bypass diodes in thejunction box shown in FIG. 14A.

DETAILED DESCRIPTION

The following detailed description should be read with reference to thedrawings, in which identical reference numbers refer to like elementsthroughout the different figures. The drawings, which are notnecessarily to scale, depict selective embodiments and are not intendedto limit the scope of the invention. The detailed descriptionillustrates by way of example, not by way of limitation, the principlesof the invention. This description will clearly enable one skilled inthe art to make and use the invention, and describes severalembodiments, adaptations, variations, alternatives and uses of theinvention, including what is presently believed to be the best mode ofcarrying out the invention.

As used in this specification and the appended claims, the singularforms “a,” “an,” and “the” include plural referents unless the contextclearly indicates otherwise. Also, the term “parallel” is intended tomean “substantially parallel” and to encompass minor deviations fromparallel geometries. The term “perpendicular” is intended to mean“perpendicular or substantially perpendicular” and to encompass minordeviations from perpendicular geometries rather than to require that anyperpendicular arrangement described herein be exactly perpendicular. Theterm “square” is intended to mean “square or substantially square” andto encompass minor deviations from square shapes, for examplesubstantially square shapes having chamfered (e.g., rounded or otherwisetruncated) corners. The term “rectangular” is intended to mean“rectangular or substantially rectangular” and to encompass minordeviations from rectangular shapes, for example substantiallyrectangular shapes having chamfered (e.g., rounded or otherwisetruncated) corners.

This specification discloses high-efficiency solar modules (alsoreferred to herein as solar panels) comprising silicon solar cellsarranged in an overlapping shingled manner and electrically connected inseries by conductive bonds between adjacent overlapping solar cells toform super cells, with the super cells arranged in physically parallelrows in the solar module. A super cell may comprise any suitable numberof solar cells. The super cells may have lengths spanning essentiallythe full length or width of the solar module, for example, or two ormore super cells may be arranged end-to-end in a row. This arrangementhides solar cell-to-solar cell electrical interconnections and increasesthe efficiency and the aesthetic attractiveness of the module.

Advantageously, the solar modules described herein include electricalinterconnects between rear surfaces of solar cells in adjacent rows ofsuper cells that provide alternative current paths (i.e., detours)through the solar panel around damaged, shaded, or otherwiseunderperforming solar cells. These detour current paths do not passthrough bypass diodes.

Turning now to the figures for a more detailed understanding of thesolar modules described in this specification, FIG. 1 shows across-sectional view of a string of series-connected solar cells 10arranged in a shingled manner with the ends of adjacent solar cellsoverlapping and electrically connected to form a super cell 100. Eachsolar cell 10 comprises a semiconductor diode structure and electricalcontacts to the semiconductor diode structure by which electric currentgenerated in solar cell 10 when it is illuminated by light may beprovided to an external load.

In the examples described in this specification, each solar cell 10 is arectangular crystalline silicon solar cell having front (sun side)surface and rear (shaded side) surface metallization patterns providingelectrical contact to opposite sides of an n-p junction, the frontsurface metallization pattern is disposed on a semiconductor layer ofn-type conductivity, and the rear surface metallization pattern isdisposed on a semiconductor layer of p-type conductivity. However, othermaterial systems, diode structures, physical dimensions, or electricalcontact arrangements may be used if suitable. For example, the front(sun side) surface metallization pattern may be disposed on asemiconductor layer of p-type conductivity, and the rear (shaded side)surface metallization pattern disposed on a semiconductor layer ofn-type conductivity.

Rectangular solar cells 10 may be prepared, for example, by separating astandard sized square or pseudo-square solar cell wafer into two or more(i.e., N) rectangular solar cells each having a length equal to the sidelength (e.g., 156 millimeters) of the standard sized solar cell waferand a width equal to a fraction (i.e., about 1/N) of the side length ofthe standard sized solar cell wafer. N may be, for example, 2 to 20 ormore, for example 6 or 8.

Referring again to FIG. 1 , in super cell 100 adjacent solar cells 10are conductively bonded directly to each other in the region in whichthey overlap by an electrically conductive bonding material thatelectrically connects the front surface metallization pattern of onesolar cell to the rear surface metallization pattern of the adjacentsolar cell. Suitable electrically conductive bonding materials mayinclude, for example, electrically conductive adhesives and electricallyconductive adhesive films and adhesive tapes, and conventional solders.

FIG. 2 shows a front view of an example rectangular solar module 200comprising six rectangular super cells 100, each of which has a lengthapproximately equal to the length of the long sides of the solar module.The super cells are arranged as six parallel rows with their long sidesoriented parallel to the long sides of the module. A similarlyconfigured solar module may include more or fewer rows of suchside-length super cells than shown in this example. In other variationsthe super cells may each have a length approximately equal to the lengthof a short side of a rectangular solar module, and be arranged inparallel rows with their long sides oriented parallel to the short sidesof the module. In yet other arrangements each row may comprise two ormore super cells, which may be electrically interconnected in series forexample. The modules may have shorts sides having a length, for example,of about 1 meter and long sides having a length, for example, of about1.5 to about 2.0 meters. Any other suitable shapes (e.g., square) anddimensions for the solar modules may also be used. A super cell maycomprise any suitable number of rectangular solar cells of any suitabledimensions. Similarly, a row of super cells may comprise any suitablenumber of rectangular solar cells of any suitable dimensions arranged inone or more super cells.

Solar modules as described herein typically comprise many more (e.g., Ntimes) as many solar cells as a conventional module of the same sizebecause N rectangular solar cells are formed from a single conventionalsized solar cell wafer. Optionally, the super cells formed from thesesolar cells may be arranged in an electrically parallel/seriescombination that provides current and voltage outputs similar to thoseprovided by a solar module of about the same size comprisingseries-connected conventional size solar cells. For example, if aconventional module includes M conventional size solar cellselectrically connected in series, then a corresponding shingled supercell module comprising N electrically parallel rows of super cells witheach super cell row comprising M series connected rectangular solarcells (each having 1/N the area of a conventional solar cell) wouldprovide about the same voltage and current output as the conventionalmodule.

The example solar modules of FIG. 2 and of FIGS. 3-11 (described below)comprise six rows of super cells all of which are electricallyinterconnected in parallel by terminal interconnects 250 at oppositeends of the rows. Because of the electrically parallel arrangement, thevoltage across each row (voltage between one end of the row and theother) is the same though the current through each row may be different.“Detour” electrical interconnect arrangements similar to those describedbelow with respect to FIGS. 3-11 may also be employed in solar modulescomprising fewer rows of super cells and/or in which some but not allrows of super cells are electrically connected in parallel.

Typically, though not necessarily, the solar modules described hereincomprise one or more (e.g., three) bypass diodes. If a solar cellarranged electrically in parallel with one of the bypass diodessignificantly limits current due to shading, cracking, or otherwisesuboptimal cell performance, the bypass diode will become forward biasedand electrically bypass that solar cell or a portion of the moduleincluding that solar cell. This prevents formation of a dangerous hotspot around the current limiting cell and improves performance of themodule.

Because the solar modules described herein include super cellselectrically connected in parallel, there is an opportunity to improveperformance further by providing alternate current paths (i.e. detours)so that in the event that one cell in a super cell is severely shaded orotherwise current limiting an adjacent string of cells in anelectrically parallel super cell can try to compensate by operating at ahigher current. These detour paths pass through the rear surfacemetallization of solar cells and through detour electrical interconnectsthat electrically connect equal voltage pairs of solar cells locatedside-by-side in adjacent super cell rows in the module. Conductionthrough the rear surface metallization of the solar cells enable thebypass and detour architectures using detour interconnects and/or planarpatterned metallized back sheets described herein.

In the extreme case all rows of super cells are electrically connectedin parallel and every solar cell would have detour connectors attachedto at least one cell in a different (e.g., adjacent) row to providealternative current paths. However, detour connectors can instead beplaced on a subset of cells to statistically reduce the likelihood thatdamage from cracking or other failure mechanisms significantly degradesperformance of the module.

Furthermore, detour connections can be concentrated in areas of themodule most likely to experience cell cracking, such as for examplealong well know stress lines from mechanical loading. Cracks can becreated by several mechanisms, may be dependent on the way the module ismounted in the field or on the roof, and may occur in predictablepatterns based on the mounting method and the source of stress. Wind andsnow load create specific stress and hence cracking. Walking on themodule may create cracks. Severe hail may create another type of crack.While initially cracks may not cause electrical disconnects or otherwisedegrade a module's performance, the cracks may expand as the module goesthough heating and cooling cycles and eventually significantly affectmodule performance. Cracks in monocrystalline and polycrystalline cellsmay behave differently.

The detour electrical connections between the rear surface metallizationon solar cells in adjacent rows may be made, for example, using shortcopper interconnects that bridge a gap between the rows and that areconductively bonded at opposite ends to the rear surfaces of the solarcells. The detour interconnects may be bonded to the solar cells (e.g.,to contact pads on the rear surface of the solar cells) using solder orconductive glue or other conductive adhesive, for example, or by anyother suitable method. Any portion of a detour interconnect that wouldotherwise be visible from the front of the solar module (i.e., through agap between rows) may be covered with a black coating or black tape, orotherwise darkened or hidden, to preserve an “all black” look from afront view of the module. In operation, the conductive detour currentpath may include portions of the rear surface (e.g., aluminum) cellmetallization as well as the detour interconnect.

Alternatively, the detour interconnections between solar cells in a“line” of solar cells oriented perpendicularly to the super cell rowsmay be made for example with a single long approximately module-widthcrossing ribbon that is conductively bonded to the rear surface of eachcell in the line. This approach may be preferred for example for modulesincluding very large numbers of solar cells, for example a module havingsix rows of super cells with each row having eighty solar cells. Such amodule would otherwise require 400 separate short interconnects toprovide detour paths for each cell.

The detour interconnections (short or long) may be made in the same wayas “hidden tap” interconnections to bypass diodes, as described forexample in U.S. patent application Ser. No. 14/674,983 titled “ShingledSolar Cell Panel Employing Hidden Taps” filed Mar. 31, 2015, which isincorporated herein by reference in its entirety. The '983 applicationalso discloses rear surface metallization patterns and contact pads forhidden tap interconnections to bypass diodes that facilitate detourinterconnections as described herein as well. As shown in FIGS. 3-11 ,for example, the detour paths and the connections to bypass diodes in asolar module may be made using the same or substantially similar typesof interconnects.

The detour interconnections may also be made, for example, using apatterned metallized back sheet conductively bonded to the rear surfacesof the solar cells, with the patterned metallization on the back sheetproviding the detour current interconnections. The patternedmetallization on the back sheet may also provide electrical connectionsto bypass diodes and/or to a junction box. (See discussion of FIGS.14A-14B below, for example). Typically, the metallization pattern on theback sheet is single layer planar.

In the example solar module 300 of FIG. 3 , all available detour pathsare installed. That is, the rear surface metallization of each solarcell 10 is electrically connected to the rear surface metallization ofits neighbor solar cell (or solar cells) in adjacent super cell rows bydetour interconnectors 275. Two of the detour interconnections (275A and275B) are also electrically connected via return wires (conductors) 280Aand 280B to three bypass diodes (not shown) in junction box 290. Returnwires 280C and 280D electrically connect the bypass diodes to terminalinterconnects 250. The other detour interconnections in line across therows with detour interconnect 275A or 275B serve as hidden taps to thebypass diodes in addition to providing detour current paths. (Similararrangements with detour interconnects also providing hidden taps tobypass diodes are shown in other figures, as well).

In FIG. 3 and the other figures described below, it should be understoodthat return wires such as 280A-280D, for example, are electricallyinsulated from the solar cells and conductors over which they pass,except at their ends. For example, return wire 280B in FIG. 3 iselectrically connected (e.g., conductively bonded) to detour electricalinterconnect 275B but electrically insulated from the other detourelectrical interconnects over which it passes on the way to junction box290. This may be accomplished for example with a strip of insulationplaced between the return wire and the rear surfaces of the solar cellsand other module components.

The example solar module 400 of FIG. 4 is similar to that of FIG. 3 ,except that in solar module 400 every other (i.e., alternating) solarcell along a super cell row has detours installed.

In example solar module 500 of FIG. 5 , detour interconnects 275 areinstalled in a pattern designed to compensate for a typical crackpattern that may result from uniform mechanical loading of a solarmodule. The crack pattern is shown in FIG. 13 superimposed on a sketchof a conventional ribbon tabbed solar module, with the crack patterngenerally indicated by lines 305. In the example of FIG. 5 , conductors280A and 280B are conductively bonded to the rear surface metallizationof solar cells 10A and 10B, respectively, to electrically connect themto bypass diodes in junction box 290

Detour interconnects may be installed at any suitable intervals along asuper cell row. The intervals may be equal or approximately equal, orinstead vary in length along the row. In example solar modules 600 (FIG.6 ) and 700 (FIG. 7 ), detour interconnects 275 are installed in fourapproximately evenly spaced lines across the module. In example solarmodules 800 (FIG. 8 ) and 900 (FIG. 9 ), detour interconnects 275 areinstalled in five lines across the module, with the interval betweendetour interconnects greater at one end of the module than at the otherend of the module. In example solar module 1000 (FIG. 10 ), detourinterconnects 275 are installed in six lines across the module, with theinterval between interconnects greater in the central portion of themodule than at the ends of the module. In example solar module 1100(FIG. 11 ), detour interconnects 275 are installed in nine lines acrossthe module in combination with five series-connected bypass diodes, withtwo lines of interconnects between each adjacent pair of bypass diodes.

If the solar module comprises bypass diodes, any suitable number ofbypass diodes may be used and they may be spaced along the super cellrows at any suitable interval. The bypass diodes may be installed in ajunction box, or alternatively embedded in a laminate comprising thesolar cells. Example solar modules 300, 400, 500, and 1000 each includethree series-connected bypass diodes (not shown) arranged in junctionbox 290. In example solar modules 600, 700, 900, and 1100 fiveseries-connected bypass diodes 310 are embedded in the solar celllaminate. In example solar cell module 800 three series-connected bypassdiodes 310 are embedded in the laminate. Example solar modules 700 and900 each include two junction boxes 290A and 290B, one at each end ofthe module, each providing a single (e.g., positive or negative) output.

Referring now to FIGS. 12A-12B, a crack (e.g., crack 330) oriented alongthe long axis of a solar cell 10 can substantially reduce current flowperpendicular to the long axis of the cell, which is the direction inwhich current generally and preferably flows through the solar cellsduring normal operation of the modules described herein (i.e., when nottaking a detour path). The use of detour electrical interconnects asdescribed above can provide a detour path around the cracked cell.

A detour current path around and over the crack can also be providedwithin the cell, as shown in FIGS. 12A-12B. In particular, detourinterconnect contact pads 320 on the rear surface of the solar cell arepositioned at the short ends of the solar cell and elongated parallel tothe short ends to substantially span the width of the solar cell. Detourinterconnects 275 that are conductively bonded to these contact padsprovide a crack jumping current path, allowing current within the cellto make its way to an interconnect 275, go over or around the crack, andthen back to the other part of the solar cell as shown for example byarrows 335.

Referring now to FIGS. 14A-14B, example patterned metallized back sheet350 provides detour current paths and electrical connections to bypassdiodes 310 in a junction box 290 corresponding to those provided bydetour interconnects 275 and return wires 280A-280D shown in FIG. 10 .(The junction box is not part of the back sheet, but is located in themodule with respect to the back sheet as shown in the figures). Inparticular, the metallization pattern comprises a positive return region355, a negative return region 360, a first bypass diode return path 365,a second bypass diode return path 370, two rows of detour interconnectregions 375A that also serve as hidden taps to the bypass diodes, andthree additional rows of detour interconnect regions 375B. Metallizationis removed from the sheet, for example as indicated at 380, toelectrically isolate the various regions from each other.

Although in the example solar modules described above each rectangularsolar cell 10 has long sides having a length equal to the side length ofa conventional silicon solar cell wafer, alternatively the long sides ofsolar cells 10 can be a fraction (e.g., ½, ⅓, ¼, or less) of the sidelength of a conventional solar cell wafer. The number of rows of supercells in a module can be correspondingly increased, for example by thereciprocal of that fraction (or by one or more rows less than thereciprocal to leave room for gaps between rows). For example, each fulllength solar cell 10 in solar module 300 (FIG. 3 ) could be replaced bytwo solar cells of ½ length arranged in eleven or twelve rows of supercells, or in any other suitable number of rows of super cells. Therectangular solar cells could have dimensions of ⅙ by ½ the side lengthof a conventional solar cell wafer, for example. Reducing cell length inthis manner may increase the robustness of the cells with respect tocracking, and reduce the impact of a cracked cell on performance of themodule. Further, the use of detour electrical interconnects ormetallized backing sheets as described above with smaller cells as justdescribed can increase the number of detour current paths availablethrough the module (compared to the use of full length cells), furtherreducing the impact of a cracked cell on performance.

This disclosure is illustrative and not limiting. Further modificationswill be apparent to one skilled in the art in light of this disclosureand are intended to fall within the scope of the appended claims.

What is claimed is:
 1. A solar module comprising: a first, second, andthird super cell arranged in physically parallel rows, each super cellcomprising a plurality of crystalline silicon solar cells, eachcrystalline silicon solar cell having a front surface metallizationpattern on a front surface and a rear surface metallization pattern on arear surface to provide electrical contact to opposite sides of thecrystalline silicon solar cell; wherein the plurality of crystallinesilicon solar cells in each super cell are arranged in an overlappingshingled manner and conductively bonded to each other in a region inwhich they overlap to electrically connect the crystalline silicon solarcells in series; a first and second terminal electrical interconnectlocated at a first and second end of the solar module, respectively, andelectrically connecting the first, second, and third super cells inparallel; a first detour electrical interconnect arranged to extendalong a first line perpendicular to the first, second, and third supercells arranged in physically parallel rows, the first detour electricalinterconnect electrically connecting the rear surface metallizationpatterns on the rear surfaces of crystalline silicon solar cells in thefirst, second, and third super cells located along the first line; asecond detour electrical interconnect arranged to extend along a secondline perpendicular to the first, second, and third super cells arrangedin physically parallel rows, the second detour electrical interconnectelectrically connecting the rear surface metallization patterns on therear surfaces of crystalline silicon solar cells in the first, second,and third super cells located along the second line; a junction boxcontaining a bypass diode; a first return conductor electricallyconnecting the first detour electrical interconnect to the bypass diodein the junction box; and a second return conductor electricallyconnecting the second detour electrical interconnect to the bypass diodein the junction box, the second return conductor crossing the firstline, the second return conductor separate from the first returnconductor.
 2. The solar module of claim 1, wherein the first and seconddetour electrical interconnects are spaced apart from each other atequal intervals along the solar module.
 3. The solar module of claim 1,wherein the junction box provides a single positive or negative outputfor the solar module.
 4. The solar module of claim 1 comprising a secondbypass diode, wherein the junction box contains the second bypass diode.5. The solar module of claim 4, comprising a third return conductor, thethird return conductor electrically connecting the first terminalelectrical interconnect to the second bypass diode in the junction box.6. The solar module of claim 5, wherein the first return conductor iselectrically connected to the second bypass diode.
 7. The solar moduleof claim 1, wherein each detour electrical interconnect is or comprisesa conductive ribbon electrically connected to the rear surfacemetallization pattern on the rear surface of a crystalline silicon solarcell in each row.
 8. The solar module of claim 1, wherein the rearsurface metallization pattern of each crystalline silicon solar cellcomprises a rear detour interconnect contact pad on the rear surface ofthe crystalline silicon solar cell.
 9. The solar module of claim 8,wherein the rear detour interconnect contact pad is elongated in adirection parallel to a short side of the crystalline silicon solarcell.
 10. The solar module of claim 1, wherein the bypass diode isconnected in parallel to 22 or more crystalline silicon solar cells inthe first super cell.
 11. The solar module of claim 1, wherein thebypass diode is connected in parallel to 26 or more crystalline siliconsolar cells in the first super cell.
 12. The solar module of claim 1,wherein the first, second, and third super cells each contain 80 or morecrystalline silicon solar cells arranged in an overlapping shingledmanner and conductively bonded to each other.
 13. The solar module ofclaim 1, wherein the solar module contains only three bypass diodes. 14.The solar module of claim 12, wherein the solar module contains onlythree bypass diodes.
 15. The solar module of claim 6, wherein the bypassdiode is connected in parallel to 22 or more crystalline silicon solarcells in the first super cell.
 16. The solar module of claim 15, whereinthe junction box provides a single positive or negative output for thesolar module.
 17. The solar module of claim 16, wherein the first,second, and third super cells each contain 80 or more crystallinesilicon solar cells arranged in an overlapping shingled manner andconductively bonded to each other.
 18. The solar module of claim 17,wherein the solar module contains only three bypass diodes.